CN205469869U - Releasing mechanism of unmanned aerial vehicle system of launching - Google Patents
Releasing mechanism of unmanned aerial vehicle system of launching Download PDFInfo
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- CN205469869U CN205469869U CN201620085915.1U CN201620085915U CN205469869U CN 205469869 U CN205469869 U CN 205469869U CN 201620085915 U CN201620085915 U CN 201620085915U CN 205469869 U CN205469869 U CN 205469869U
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- aerial vehicle
- unmanned aerial
- release
- back box
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- 230000007246 mechanism Effects 0.000 title claims abstract description 21
- 230000006378 damage Effects 0.000 abstract description 5
- 208000027418 Wounds and injury Diseases 0.000 abstract description 4
- 208000014674 injury Diseases 0.000 abstract description 4
- 230000008878 coupling Effects 0.000 abstract description 3
- 238000010168 coupling process Methods 0.000 abstract description 3
- 238000005859 coupling reaction Methods 0.000 abstract description 3
- 230000006872 improvement Effects 0.000 abstract description 2
- 241000196324 Embryophyta Species 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
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- 235000009566 rice Nutrition 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
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Abstract
The utility model relates to an unmanned aerial vehicle release equipment field, concretely relates to releasing mechanism of unmanned aerial vehicle system of launching, collude first including supporting end box, releasing, release colludes second, upper cover plate and switching piece, release is colluded first and is passed through spring coupling in the fixed column first of the ten heavenly stems, release is colluded second and is passed through spring coupling in the fixed column second of the ten heavenly stems, be equipped with hole A and hole B on the support end box, act as go -between hole A and hole B couples together through external, the upper cover plate passes through the screw fixation on supporting end box, the switching is equipped with hole C and hole D on the piece, and the release problem of the solve unmanned aerial vehicle system of launching is launched the releasing mechanism of system with the unmanned aerial vehicle that has now and is compared, the utility model discloses more smooth and easy when launching, very big improvement the probability of success of unmanned aerial vehicle catapult -assisted take -off, operating personnel can keep away from ejection mechanism simultaneously, the unexpected injury that has brought to operating personnel when effectively having avoided launching the system trouble.
Description
Technical field
This utility model relates to unmanned plane release device field, is specifically related to a kind of unmanned aerial vehicle ejecting system
Relieving mechanism.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is to utilize radio distant
The most manned aircraft that control equipment and the presetting apparatus provided for oneself are handled.Can divide from technical standpoint definition
For: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned umbrella
Wing machines etc., unmanned plane is pressed application, can be divided into military and civilian.Military aspect, unmanned plane is divided into
Reconnaissance plane and target drone, unmanned plane+sector application, is real just the needing of unmanned plane.At present taking photo by plane, agriculture
The application in the fields such as industry plant protection, mapping, has greatly expanded the purposes of unmanned plane itself.
Along with social development, unmanned plane is more and more extensive in the application of every field.Currently on the market
The unmanned plane sold, its mode of taking off is generally divided into rolling start and catapult-assisted take-off, and launching cradle is one
It is about the track of 4-6 rice, a mechanism that can slide installed above.Unmanned plane body is arranged on cunning
On motivation structure, rely on the mode such as elastic or compressed air by airplane catapult to takeoff speed.Existing
Relieving mechanism design is loaded down with trivial details, and in ejection process, fault rate is the highest, and body can be produced structural damage
Hinder and cause aircraft to be scrapped.
Utility model content
For problem above, this utility model provides the relieving mechanism of a kind of unmanned aerial vehicle ejecting system,
Solve the release And Spread of Solute of unmanned aerial vehicle ejecting system, with existing unmanned aerial vehicle ejecting system relieving mechanism phase
Ratio, this utility model is more smoothly when launching, and greatly improves the success that unmanned aerial vehicle ejecting takes off
Probability, simultaneously operator can away from ejection mechanism, effectively prevent when ejection system breaks down to
The unexpected injury that operator bring, can effectively solve the problem in technical background.
To achieve these goals, the technical solution adopted in the utility model is as follows: a kind of unmanned plane bullet
Penetrating the relieving mechanism of system, including supporting back box, release hook first, release hooks second, upper cover plate and switching
Sheet, described release is hooked first and is connected in fixing post first by spring, and described release hooks second by spring even
Being connected in fixing post second, described support back box is provided with hole A and hole B, described hole A and is drawn by external
Line couples together with hole B, and described upper cover plate is screwed in support back box, described switching piece
It is provided with hole C and hole D.
Further, it is additionally provided with limited post in described support back box.
Further, described release hooks first and is provided with lug first and lug second.
Further, a side opening of described support back box is provided with support back box opening, described support
Back box opening be shaped as rectangle.
The beneficial effects of the utility model:
This utility model solves the release And Spread of Solute of unmanned aerial vehicle ejecting system, with existing unmanned aerial vehicle ejecting
System relieving mechanism is compared, and this utility model is more smoothly when launching, and greatly improves unmanned plane
The probability of success of catapult-assisted take-off, operator can effectively prevent to launch away from ejection mechanism be simultaneously
The unexpected injury that system brings to operator when breaking down.
Accompanying drawing explanation
Fig. 1 this utility model structural representation.
Fig. 2 this utility model supports back box structural representation.
Fig. 3 this utility model supports the top view of back box.
The release of Fig. 4 this utility model hooks first structural representation.
The release of Fig. 5 this utility model hooks second structural representation.
Fig. 6 this utility model upper cover plate structural representation.
Fig. 7 this utility model switching piece structural representation.
Being numbered in figure: 1-supports back box, 2-release hooks first, and 3-release hooks second, 4-upper cover plate, 5-
Switching piece, 6-fixes post first, and 7-fixes post second, 8-limited post, 9-hole A, 10-lug first, 11-
Lug second, 12-hole B, 13-hole C, 14-hole D, 15-support back box opening.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with
Drawings and Examples, are further elaborated to this utility model.Should be appreciated that this place is retouched
The specific embodiment stated, only in order to explain this utility model, is not used to limit this utility model.
As shown in Figures 1 to 7, the relieving mechanism of a kind of unmanned aerial vehicle ejecting system, including supporting back box
1, release hooks first 2, and release hooks second 3, upper cover plate 4 and switching piece 5, and described release hooks first 2 and passes through
Spring is connected in fixing post first 6, and described release is hooked second 3 and is connected in fixing post second 7 by spring,
Described support back box 1 is provided with hole A9 and hole B12, described hole A9 by external bracing wire and hole B12
Coupling together, described upper cover plate 4 is screwed in support back box 1, on described switching piece 5
It is provided with hole C13 and hole D14.
On above-described embodiment preferably, it is additionally provided with limited post 8 in described support back box 1.
On above-described embodiment preferably, described release hooks first 2 and is provided with lug first 10 and lug second 11.
On above-described embodiment preferably, a side opening of described support back box 1 is provided with support back box and opens
Mouthfuls 15, described support back box opening 15 be shaped as rectangle.
When this utility model uses, by the hole C13 on switching piece 5 towards the side supported within back box 1
To, from supporting honest at back box opening 15 being inserted into inwards between lug first 10 and lug second 11
In arcuate groove, push hard on earth, this completes and of the present utility model launch preparation.Need
Pull external release bracing wire when launching thus drive release to hook second 3 and be turned out, and then make release hook first 2
Out of hand, release hook first 2 moves downward under the action of the spring, makes switching piece 5 be released,
It is finally completed launching of unmanned plane.
Based on above-mentioned, this utility model solves the release And Spread of Solute of unmanned aerial vehicle ejecting system, with existing
Unmanned aerial vehicle ejecting system relieving mechanism is compared, and this utility model is more smoothly when launching, and carries greatly
The probability of success that high unmanned aerial vehicle ejecting takes off, operator effectively can keep away away from ejection mechanism simultaneously
Exempt from the unexpected injury brought when ejection system breaks down to operator.
The foregoing is only preferred embodiment of the present utility model, not new in order to limit this practicality
Type, all any amendment, equivalent and improvement made within spirit of the present utility model and principle
Deng, within should be included in protection domain of the present utility model.
Claims (4)
1. the relieving mechanism of a unmanned aerial vehicle ejecting system, it is characterised in that: include supporting back box, releasing
Putting hook first, release hooks second, upper cover plate and switching piece, and described release hooks first and is connected to fix by spring
In post first, described release is hooked second and is connected in fixing post second by spring, and described support back box is provided with
Hole A and hole B, described hole A are coupled together with hole B by external bracing wire, and described upper cover plate passes through spiral shell
Silk is fixed in support back box, and described switching piece is provided with hole C and hole D.
The relieving mechanism of a kind of unmanned aerial vehicle ejecting system the most according to claim 1, its feature exists
In: it is additionally provided with limited post in described support back box.
The relieving mechanism of a kind of unmanned aerial vehicle ejecting system the most according to claim 1, its feature exists
In: described release hooks first and is provided with lug first and lug second.
The relieving mechanism of a kind of unmanned aerial vehicle ejecting system the most according to claim 1, its feature exists
In: a side opening of described support back box is provided with support back box opening, described support back box opening
It is shaped as rectangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620085915.1U CN205469869U (en) | 2016-01-26 | 2016-01-26 | Releasing mechanism of unmanned aerial vehicle system of launching |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620085915.1U CN205469869U (en) | 2016-01-26 | 2016-01-26 | Releasing mechanism of unmanned aerial vehicle system of launching |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205469869U true CN205469869U (en) | 2016-08-17 |
Family
ID=56619023
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620085915.1U Expired - Fee Related CN205469869U (en) | 2016-01-26 | 2016-01-26 | Releasing mechanism of unmanned aerial vehicle system of launching |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205469869U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019080185A1 (en) * | 2017-10-27 | 2019-05-02 | 罗伟 | Unmanned aerial vehicle release mechanism and fixed-wing unmanned aerial vehicle |
-
2016
- 2016-01-26 CN CN201620085915.1U patent/CN205469869U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019080185A1 (en) * | 2017-10-27 | 2019-05-02 | 罗伟 | Unmanned aerial vehicle release mechanism and fixed-wing unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160817 |